# N3322L: 1967 Douglas DC-9-32, registration cancelled 2013-02-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 6, 2013 - Status when cancelled: Second renewal notice - Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47031 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 11, 1981 - Certificate issued: November 9, 2007 - Last registry action: April 3, 2012 - Mode S code: A39FE6 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N3322L - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=3322L - Page: https://openairdocs.org/deregistered/N3322L-2013-02-06 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-9-32: https://openairdocs.org/model/douglas-dc-9-32.md ## Service difficulty reports (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1227889940](https://openairdocs.org/sdr/DALA1227889940), Apr 28, 2012: CAM. WORN. COMPLIED WITH FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM. FOUND RELEASE CAM BASE WORN IN 2 SPOTS. FAILED TORQUE CHECK REPLACED BASE. - [SDR 0301979940](https://openairdocs.org/sdr/0301979940), Oct 28, 2003: CONTROLLER. MALFUNCTIONED. DURING CLIMBOUT, A BURNING ODOR AND LIGHT HAZE PERMEATED THE CABIN. THE LT PACK VALVE WAS PEGGED FULL RT AND THE LT DUCT TEMPERATURE REACHED 120 DEGREES. FLIGHT - [SDR 0203949940](https://openairdocs.org/sdr/0203949940), Nov 13, 2002: DOOR FRAME. CRACKED. DURING AN OVERNIGHT CHECK, A CRACK WAS FOUND IN THE AFT PRESSURE BULKHEAD DOORJAMB. THE AIRCRAFT WAS FERRIED TO ACCOMPLISH REPAIRS. THE CRACK WAS 2 INCHES LONG - [SDR 0003999940](https://openairdocs.org/sdr/0003999940), Oct 18, 2000: ATTACH ANGLE. CRACKED. DURING L-CHECK, FOUND CRACK IN RIGHT HAND PYLON UPPER ATTACH ANGLE AT BS 996. REPAIRED PER EA 99-17403 AND SRM 54-04 FIGURE 10. REF LOG PAGE 1510889. - [SDR 9903389940](https://openairdocs.org/sdr/9903389940), Aug 22, 1999: TIRE. FAILED. ON TAKEOFF APROXIMATELY AT ROTATION SPEED, THE RIGHT ENGINE COMPRESSOR STALLED, EGT AND EPR INDICATIONS FLUCTUATED, AND A BURNING RUBBER SMELL WAS REPORTED IN T - [SDR 9808129940](https://openairdocs.org/sdr/9808129940), May 1, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9802169940](https://openairdocs.org/sdr/9802169940), Feb 3, 1998: PROX SENSOR. BROKEN. NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND FLIGHT CONTINUED TO DESTINATION. ON GEA - [SDR 9801019940](https://openairdocs.org/sdr/9801019940), Jan 18, 1998: BATTERY. DISCHARGED. DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LIGHTS BATTERY LOW. REPLACED SLIDE. - [SDR 9800999940](https://openairdocs.org/sdr/9800999940), Jan 18, 1998: BATTERY. DISCHARGED. DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LIGHTS BATTERY LOW. REPLACED SLIDE. - [SDR 9801869940](https://openairdocs.org/sdr/9801869940), Jan 15, 1998: BULKHEAD. CRACKED. DURING L CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE LEFT OUTBOARD VERTICAL SUPPORT FS 108. REPAIRED PER EA 99-153 - [SDR 9801859940](https://openairdocs.org/sdr/9801859940), Jan 15, 1998: BULKHEAD. CRACKED. DURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD AND INBOARD VERTICAL SUPPORTS FS 108. REPAIRED - [SDR 9721599940](https://openairdocs.org/sdr/9721599940), Nov 16, 1997: RELAY. INOPERATIVE. DURING LINE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED R2-213 RELAY, OPERATIONAL CHECK OK. - [SDR 9716729940](https://openairdocs.org/sdr/9716729940), Sep 3, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EMERGENCY EXIT LIGHT VERY DIM DURING TEST. REPLACED BATTERY PACK AND BATTERIES. OPERATIONAL CHECK N - [SDR 9716709940](https://openairdocs.org/sdr/9716709940), Aug 29, 1997: UPLATCH MECH. FAILED. ON DEPARTURE AT 11,000 FEET AND 310 KNOTS, A 'THUD' WAS FELT IN THE AIRFRAME ALONG WITH NOISE OF THE GEAR DOORS OPENING SUDDENLY. RIGHT HYDRAULIC SYSTEM WAS PRE - [SDR 9715399940](https://openairdocs.org/sdr/9715399940), Aug 11, 1997: DOWNLOCK SW. MALFUNCTIONED. DURING APPROACH, RIGHT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND CONFIRMED VISUALLY THROUGH PERISCO - [SDR 9713749940](https://openairdocs.org/sdr/9713749940), Jul 11, 1997: BATTERIES. DISCHARGED. FLIGHT ATTENDANT REPORTED AFT EMERGENCY FLASHLIGHT NOT BLINKING. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9709189940](https://openairdocs.org/sdr/9709189940), May 7, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CH - [SDR 9705429940](https://openairdocs.org/sdr/9705429940), Mar 15, 1997: CLIP. OUT OF ADJUST. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, OPERATIONAL CHECK OK. - [SDR 9700739940](https://openairdocs.org/sdr/9700739940), Jan 10, 1997: EPR TRANSMITTER. MALFUNCTIONED. AS TAKEOFF POWER WAS APPLIED, BOTH ENGINE EPR INDICATIONS FROZE AT 1.60. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMI - [SDR 9700729940](https://openairdocs.org/sdr/9700729940), Jan 10, 1997: PT7 LINE. WATER CONTAM. AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EPR INDICAITON DID NOT RESPOND. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED MOISTURE F - [SDR 9627109940](https://openairdocs.org/sdr/9627109940), Dec 28, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9625049940](https://openairdocs.org/sdr/9625049940), Nov 19, 1996: PITOT LINE. BLOCKED. RUDDER TRAVEL UNRESTRICTED LIGHT REMAINED ON AFTER TAKEOFF. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PITOT LINE TO RUDDER LIMITER P - [SDR 9623709940](https://openairdocs.org/sdr/9623709940), Nov 6, 1996: WIRE. MISINSTALLED. DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRES AT CANNON PLUG RECEPTACLES R5-4009 PINS L AND M - [SDR 9620339940](https://openairdocs.org/sdr/9620339940), Sep 20, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK AND CONE RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED FLOOD LIGHT/POWER SUPPLY ASSEM - [SDR 9618869940](https://openairdocs.org/sdr/9618869940), Aug 26, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND BOTH LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9618409940](https://openairdocs.org/sdr/9618409940), Aug 24, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EVACUATION LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9615779940](https://openairdocs.org/sdr/9615779940), Jul 18, 1996: CONTROLLER. MALFUNCTIONED. LOSS OF CABIN PRESSURIZATION OCCURRED DURING INITIAL DESCENT AT 31,000 FEET. EMERGENCY DESCENT WAS MADE TO 10,000 FEET AND CABIN PRESSURE WAS REGAINED. FLIGHT C - [SDR 9616449940](https://openairdocs.org/sdr/9616449940), Jul 2, 1996: LONGERON. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE RIGHT WING STR 14 AT XRS 68 AND ON STR 19 AT XRS 60. REPAIRED STRINGERS (P/N 5919238-502, 5911279-502) PER EA 99-110820, - [SDR 9614829940](https://openairdocs.org/sdr/9614829940), Jul 2, 1996: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE FITTING LOCATED AT WING STR 15 AND THE RIGHT WS 69 FRAME. REPLACED FITTING PER SRM 51-30-5. - [SDR 9616439940](https://openairdocs.org/sdr/9616439940), Jul 1, 1996: LONGERON. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE LEFT WING STR 13 TO 15, 17 BETWEEN XW 58 AND XRS 112. REPAIRED STRINGER (P/N 5919239, 5919237, 5919238) PER EA 99-110827. - [SDR 9615329940](https://openairdocs.org/sdr/9615329940), Jun 30, 1996: SPLICE. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE LOWER FORWARD SPAR CAP SPLICE PLATE AT XRS 91, LEFT SIDE. REPAIRED SPLICE (P/N 3912208-1) PER EA 99-109071. - [SDR 9611859940](https://openairdocs.org/sdr/9611859940), May 28, 1996: INSULATION. OUT OF POSITION. AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE INSULATION BLANKET STUCK IN OUTFLOW VAL - [SDR 9613969940](https://openairdocs.org/sdr/9613969940), May 27, 1996: FRAME. CRACKED. DURING M-CHECK, FOUND THREE CRACKS ON THE FS 756 FRAME INBOARD FLANGE OF THE LOWER PRODUCTION SPLICE POCKET. REPAIRED FRAME (P/N 9919620-501) PER EA 99-108562. - [SDR 9613959940](https://openairdocs.org/sdr/9613959940), May 27, 1996: SILL. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE LEFT HAND WINDOW FRAME SILL, UPPER SIDE, BETWEEN FS 389 TO 408. REPAIRED SILL PER EA 99-108554. - [SDR 9611809940](https://openairdocs.org/sdr/9611809940), May 27, 1996: FITTING. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE FRONT SPAR FITTING AT FS 598 TO 617 LBL 66. REPLACED FITTING PER SRM 51-30-0. - [SDR 9611059940](https://openairdocs.org/sdr/9611059940), May 14, 1996: FRAME. CRACKED. DURING M-CHECK, FOUND A CRACK IN THE FS 612 FRAME ATTACH FITTING AT LONGERON 17L. REPLACED FITTING PER SRM 51-10-2. - [SDR 9607419940](https://openairdocs.org/sdr/9607419940), Mar 30, 1996: OXY REGULATOR. MALFUNCTIONED. CREW OXYGEN DROPPED TO ZERO PRESSURE, FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S AND FIRST OFFICER'S OXYGEN REGULATO - [SDR 9605869940](https://openairdocs.org/sdr/9605869940), Mar 11, 1996: BATTERY. MALFUNCTIONED. A STEADY BATTERY CHARGE RATE OF 15 TO 18 AMPS WAS OBSERVED DURING CLIMBOUT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE BATTERY CHARGER, MA - [SDR 9604039940](https://openairdocs.org/sdr/9604039940), Feb 16, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND AFT CEILING EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. - [SDR 9518929940](https://openairdocs.org/sdr/9518929940), Nov 27, 1995: EEL POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FORWARD OF ROW 6 AND THE TWO EMERGENCY EXIT SIGNS BY THE MAIN CABIN DOOR AND SERVICE DOOR INOPERATIVE. REP - [SDR 9518669940](https://openairdocs.org/sdr/9518669940), Nov 15, 1995: FITTING. CRACKED. DURING MAINTENANCE CHECK, FOUND A CRACK IN THE LEFT WING FITTING STA 164 AT STR 20, OUTBOARD SIDE. REPLACED FITTING PER EA 99-10239. - [SDR 9512569940](https://openairdocs.org/sdr/9512569940), Aug 13, 1995: YAW DAMPER. MALFUNCTIONED. DURING CLIMB THROUGH 26,000 FEET WITH AUTO-PILOT ENGAGED, THE AIRCRAFT SUDDENTLY YAWED TO ONE SIDE THEN THE OTHER. DISCONNECTED AUTO-PILOT AND PROBLEM CONTINUED - [SDR 9508489940](https://openairdocs.org/sdr/9508489940), May 16, 1995: SEALS. FAILED. ON APPROACH INTO MEM, PASSENGER AT ROW 16 REPORTED EXCESSIVE HEAT COMING FROM FLOOR AREA. BOTH FLOOR AND SIDEWALL WERE HOT TO TOUCH. ENGINE AND WING ANTI-ICE WE - [SDR 9503519940](https://openairdocs.org/sdr/9503519940), Mar 6, 1995: WIRE. CHAFED. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CRUISE FLIGHT AT 33,000 FEET. FLIGHT DIVERTED TO BIS AND LANDED WITHOUT INCIDENT. FOUND WIRING TO RIG ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW85IA011](https://openairdocs.org/ntsb/FTW85IA011), Oct 8, 1984: Douglas DC-9-32 (N3322L), Houston, TX, incident, no damage ## FAA accident and incident reports (4) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19881028060919I](https://openairdocs.org/incident/19881028060919I), Oct 28, 1988: Doug DC932 (N3322L), Denver, CO. Loss of cabin pressure. Oxygen masks deployed. Pressure stabilized on descent and aircraft continued to destination - [Incident 19861011062959I](https://openairdocs.org/incident/19861011062959I), Oct 11, 1986: Doug DC932 (N3322L), Memphis, TN. Disconnected left generator drive due to high temperature, then right generator failed. Unable to start APU. - [Incident 19860321018659I](https://openairdocs.org/incident/19860321018659I), Mar 21, 1986: Doug DC932 (N3322L), Memphis, TN. Green gear light did not come on for right main. Safe landing. Broken wire found inside harness. - [Incident 19841008076759I](https://openairdocs.org/incident/19841008076759I), Oct 8, 1984: Doug DC932 (N3322L), Houston, TX. Missed turn onto taxiway due to lack of sign, weather and unfamiliar area. Taxied onto active runway. Near miss 107T --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.